Paul K Amtower DeceasedMedley, WV

Paul Amtower Phones & Addresses

Keyser, WV

Social networks

Paul K Amtower

Linkedin

Work

Company: Orbital atk Jun 2000 to Dec 2008 Position: Inert operations manager

Education

Degree: Master of Business Administration, Masters School / High School: Frostburg State University 1994 to 1996

Skills

Government Contracting • Aerospace • Root Cause Analysis • Six Sigma • Dod • As9100 • Lean Manufacturing • Spc • Configuration Management • Security Clearance • Continuous Improvement • Manufacturing • Defense • Composites • Mission Assurance • Robotics • Microsoft Office • Pfmea • Design of Experiments • Supervisory Skills • Operations Management

Industries

Defense & Space

Mentions for Paul K Amtower

Paul Amtower resumes & CV records

Resumes

Paul Amtower Photo 15

Senior Mission Assurance Engineer

Location:
Keyser, WV
Industry:
Defense & Space
Work:
Orbital Atk Jun 2000 - Dec 2008
Inert Operations Manager
Northrop Grumman Corporation Jun 2000 - Dec 2008
Senior Mission Assurance Engineer
Education:
Frostburg State University 1994 - 1996
Master of Business Administration, Masters
West Virginia University 1982 - 1985
Bachelors, Chemical Engineering
Wvu Potomac State College 1980 - 1982
Associates, Associate of Arts, Engineering
Keyser High School
Potomac State College
Skills:
Government Contracting, Aerospace, Root Cause Analysis, Six Sigma, Dod, As9100, Lean Manufacturing, Spc, Configuration Management, Security Clearance, Continuous Improvement, Manufacturing, Defense, Composites, Mission Assurance, Robotics, Microsoft Office, Pfmea, Design of Experiments, Supervisory Skills, Operations Management

Publications & IP owners

Us Patents

Propellant Formulation And Projectiles And Munitions Employing Same

US Patent:
2007025, Nov 1, 2007
Filed:
Aug 18, 2005
Appl. No.:
11/207850
Inventors:
Paul Amtower - Keyser WV, US
International Classification:
C06B 33/00
US Classification:
149037000
Abstract:
A solid, heterogeneous, high performance rocket propellant, operable at high pressure with a burn rate relatively insensitive to changes in pressure and temperature. The propellant includes a binder, ammonium perchlorate particles, metal particles, and iron oxide. The ammonium perchlorate particles comprise a multimodal mixture of rounded particles having a weight mean diameter of from about 70 μm to about 110 μm and of nonrounded particles having a weight mean diameter of from about 7.5 μm to about 15 μm. In one embodiment, the propellant includes a binder formed from the reaction of a hydroxy terminated polybutadiene with a diisocyanate, ammonium perchlorate as an oxidizer, aluminum as a fuel, and iron oxide as a burn rate modifier. The propellant may also include bonding agents, curing catalysts, a plasticizer, antioxidant/peroxide scavengers, and pot life extenders.

Propellant Formulation

US Patent:
2004020, Oct 14, 2004
Filed:
Mar 10, 2003
Appl. No.:
10/383656
Inventors:
Paul Amtower - Keyser WV, US
International Classification:
C06B045/10
US Classification:
149/019400
Abstract:
A solid, heterogeneous, high performance rocket propellant, operable at high pressure with a bum rate relatively insensitive to changes in pressure and temperature, is disclosed. The propellant includes a binder formed from the reaction of a hydroxy terminated polybutadiene with a diisocyanate, ammonium perchlorate as an oxidizer, aluminum as a fuel, and iron oxide as a bum rate modifier. The ammonium perchlorate is a multimodal mixture of large particles with a weight mean diameter of about 70 to about 110 m and small particles having a weight mean diameter of about 7.5 to about 15 m. The propellant may also include bonding agents, curing catalysts, a plasticizer, antioxidant/peroxide scavengers, and pot life extenders.

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